EP3259510A1 - Appareil solénoïde - Google Patents

Appareil solénoïde

Info

Publication number
EP3259510A1
EP3259510A1 EP16752953.6A EP16752953A EP3259510A1 EP 3259510 A1 EP3259510 A1 EP 3259510A1 EP 16752953 A EP16752953 A EP 16752953A EP 3259510 A1 EP3259510 A1 EP 3259510A1
Authority
EP
European Patent Office
Prior art keywords
flexible element
armature
face
pole piece
disposed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP16752953.6A
Other languages
German (de)
English (en)
Other versions
EP3259510B1 (fr
EP3259510A4 (fr
Inventor
Brett E. NAGEL
Jonathan B. GAMBLE
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Enfield Tech Inc
Enfield Technologies Inc
Original Assignee
Enfield Tech Inc
Enfield Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Enfield Tech Inc, Enfield Technologies Inc filed Critical Enfield Tech Inc
Publication of EP3259510A1 publication Critical patent/EP3259510A1/fr
Publication of EP3259510A4 publication Critical patent/EP3259510A4/fr
Application granted granted Critical
Publication of EP3259510B1 publication Critical patent/EP3259510B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00—Magnets
    • H01F7/06—Electromagnets; Actuators including electromagnets
    • H01F7/08—Electromagnets; Actuators including electromagnets with armatures
    • H01F7/16—Rectilinearly-movable armatures
    • H01F7/1638—Armatures not entering the winding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
    • F16K1/32—Details
    • F16K1/34—Cutting-off parts, e.g. valve members, seats
    • F16K1/36—Valve members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K27/00—Construction of housing; Use of materials therefor
    • F16K27/02—Construction of housing; Use of materials therefor of lift valves
    • F16K27/029—Electromagnetically actuated valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/02—Actuating devices; Operating means; Releasing devices electric; magnetic
    • F16K31/06—Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/02—Actuating devices; Operating means; Releasing devices electric; magnetic
    • F16K31/06—Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid
    • F16K31/0644—One-way valve
    • F16K31/0655—Lift valves
    • F16K31/0658—Armature and valve member being one single element
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/02—Actuating devices; Operating means; Releasing devices electric; magnetic
    • F16K31/06—Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid
    • F16K31/0644—One-way valve
    • F16K31/0672—One-way valve the valve member being a diaphragm

Definitions

  • a solenoid converts energy to linear motion.
  • This linear motion may serve many purposes, including but not limited to operation of a mechanical switch and selective control of one or more fluid paths.
  • Solenoid-based systems exhibit varying degrees of efficiency (force per unit of supplied energy), linearity (i.e., of the efficiency curve), proportionality (i.e., of movement to suppled energy), and hysteresis effects (which result in different system response depending on whether the supplied energy is increasing or decreasing).
  • a solenoid and the system in which it is employed are typically designed to maximize one or more of these characteristics. However, designers face challenges in maximizing one or more of these characteristics while keeping others within desired tolerances.
  • FIG. 1 is a cross-sectional view of an apparatus according to some embodiments.
  • FIG. 2 is an elevational view of an apparatus according to some embodiments.
  • FIG. 3 is a bottom-side perspective view of an apparatus according to some embodiments.
  • FIG. 4 is an exploded view of an apparatus according to some embodiments.
  • FIG. 5 is an exploded view of an apparatus according to some embodiments.
  • FIG. 6 is a bottom-side perspective view of a pole piece according to some embodiments.
  • FIG. 7 is a top-side perspective view of a pole piece according to some embodiments.
  • FIG. 8 is a bottom-side cross-sectional view of a pole piece according to some embodiments.
  • FIG. 9 is a top-side cross-sectional view of a pole piece according to some embodiments.
  • FIG. 10 is a cross-sectional view of a pole piece according to some embodiments.
  • FIG. 11 is a bottom-side perspective view of a pole piece and a moving armature subassembly according to some embodiments.
  • FIG. 12 is an exploded view of a moving armature sub-assembly according to some embodiments.
  • FIG. 13 is a top-side cross-sectional view of a pole piece and a moving armature subassembly according to some embodiments.
  • FIG. 14 is a top-side cross-sectional view of a pole piece and a moving armature subassembly according to some embodiments.
  • FIG. 15 is a top-side perspective view of a moving armature sub-assembly in a housing according to some embodiments.
  • FIG. 16 is a bottom-side perspective view of a pole piece in a housing according to some embodiments.
  • FIG. 17 is a top-side cross-sectional view of a pole piece and a moving armature subassembly in a housing according to some embodiments.
  • FIG. 18 is a cross-sectional view of an apparatus according to some embodiments.
  • FIGS. 19 through 25 illustrate relationships between coil current and fluid flow for various physical and operational parameters according to some embodiments.
  • FIG. 26 is a cross-sectional view of an apparatus according to some embodiments.
  • FIG. 27 is a cross-sectional view of an apparatus according to some embodiments. DESCRIPTION
  • FIGS. 1-5 include cross-sectional, perspective and exploded views of an apparatus according to some embodiments.
  • the depicted apparatus is a solenoid valve, but embodiments are not limited thereto. Embodiments may differ from the depicted apparatus in shape, size, components, construction, and/or materials.
  • the housing (13) is ferromagnetic and is substantially cylindrical in construction.
  • the housing (13) contains a coil assembly comprising a coil (18) wound around a bobbin (16).
  • Pins (9) protrude through openings in the end of the housing (13).
  • Pins (9) are supported by the bobbin (16) and electrically connected to the coil (18).
  • an electrical connector (11) plugs onto pins (9) to supply power to the coil (18) via lead-wires (8). Implementations may utilize other types of connections to the pins (9) and to the coil (18).
  • the electrical connector (11) is retained by a molded plastic cap (22) which presses over an end of the housing (13) through which pins (9) protrude.
  • a seal (19) restricts the ingress of moisture into the cap (22).
  • the lead-wires (8) pass through two holes in the cap (22), which are sealed using cable seals (10).
  • a ferromagnetic core piece (12) is disposed within the bobbin (16), and abuts a ferromagnetic pole piece (3).
  • the core piece (12) and the pole piece (3) may comprise different materials (e.g., different grades of steel) particularly-suited to their below-described functions.
  • the core piece (12) and the pole piece (3) comprise a single integral piece.
  • the ferromagnetic pole piece (3) mates with a portion of a moving armature subassembly (5).
  • features of the pole piece (3) facilitate the advantageous positioning of the moving armature sub-assembly (5) and also provide improved operational efficiency.
  • FIGS. 6-9 include various views of the pole piece (3), while FIG. 10 provides a more detailed view of its construction.
  • a back face of the pole piece (3) i.e., the face exposed to the core piece (12)
  • a projection (31) extends from a face of the pole piece (3) opposite the back face.
  • the recess may be created on the back face prior to machining any of the internal features of the pole piece (3), and the recess is substantially filled by melting copper therewithin.
  • the material (15) may be selected for its structural as well as magnetic characteristics, as it may also provide support to the structure of the pole piece (3).
  • the internal features such as the projection (30) are subsequently created, leaving a thin portion of ferromagnetic base material at the base of the recess, as shown in FIG. 10.
  • these features may reduce and/or substantially prevent magnetic flux from passing between the outer cylindrical surface (17) of the pole piece (3) and the center pole face (23), increasing the amount of magnetic flux contributing to the axial force experienced by the moving armature sub-assembly (5). This phenomenon will be described in more detail below with respect to FIG. 18.
  • a sealed chamber (24) is created for a working fluid without requiring additional components and seals. Additionally, since such a working fluid would not contact the non-magnetic material (15), problems with fluid compatibility and corrosion may be virtually eliminated.
  • the aforementioned construction sequence i.e., create recess, fill recess with nonmagnetic support material, machine internal features
  • certain internal features of the pole piece (3) are used to locate and mate with the moving armature sub-assembly (5).
  • FIG. 11 is a perspective view of the moving armature sub-assembly (5) coupled to the pole piece (3) according to some embodiments.
  • the moving armature sub-assembly (5) comprises a ferromagnetic armature (6), a guide spring (4), a valve spring (7) and a poppet (2).
  • the poppet (2) further incorporates an elastomeric insert (14) in the center of its exposed face as shown.
  • the two disk springs (4) and (7) exhibit substantially higher stiffness in the radial direction than in the axial direction. These properties strongly constrain the armature (6) to move primarily in the axial direction.
  • the guide spring (4) is welded to the back face of the armature (6), and the valve spring (7) is retained by the poppet (2) which is inserted into the armature (6) and swaged in place.
  • FIGS. 13 and 14 illustrate the coupling of the pole piece (3) and the armature subassembly (5) according to some embodiments.
  • a portion of the projection (30) passes through an opening defined by the guide spring (4), features (31) of the projection (30) contact a center portion (41) of a first face of the guide spring (4), and an internal cylindrical surface (32) of the pole piece (3) is spaced a small distance from a widest outer cylindrical surface (61) of the armature (6).
  • An outer portion of the second face of the guide spring (4) is in contact with the arnature (6) at its outer circumference.
  • a face (71) of the valve spring (7) abuts a lower rim (33) of the pole piece (3).
  • FIG. 15 illustrates the armature sub-assembly (5) placed within the body (1)
  • FIG. 16 illustrates the pole piece (3) placed within the housing (13).
  • the body (1) is threaded onto the housing (13).
  • the body (1) incorporates a tubular orifice (20).
  • the body (1) may be made from a variety of materials including ferrous and non-ferrous metals, plastics and ceramics, depending on the requirements of the application.
  • one method of retaining the orifice (20) in the body (1) is to deform the body material around the circumference of the orifice (20). This both holds the orifice (20) in place, and creates a fluid tight seal between the body (1) and the orifice (20).
  • the orifice (20) may be held in place by ultrasonic welding, heat staking, adhesive etc.
  • the external end of the orifice (20) protrudes from the bottom face of the body (1) and may be threaded. This may create an industry-standard mounting interface.
  • the interior end of the orifice (20) has a small opening to limit the maximum flow therethrough. This design allows the maximum flow rating to be changed by using an orifice having a differently-sized internal opening, and/or by using a different combination of springs (7) and (4), which provides a different combined stiffness in the axial direction.
  • Each of springs (7) and (4) may exhibit any degree of axial stiffness. In certain implemenations, the guide spring (4) is small in diameter and it is therefore difficult for the guide spring (4) to provide significant stiffness in the axial direction without exceeding the stress limit of its constituent materials.
  • Some embodiments may therefore utilize a guide spring (4) which is very flexible in the axial direction, and a valve spring (7) which is much stiffer than the guide spring (4).
  • Embodiments may also or alternatively provide a common sub-assembly in which the guide spring (4) is attached permanently to the back of the armature (6), and the valve spring (7) is selected at the time of assembly, based on the required pressure and flow characteristics.
  • a wave washer (21) positioned between the body (1) and the valve spring (7) is used to press the valve spring (7) into contact with the pole piece (3) and to press the pole piece (3) against an end face of the center pole (12).
  • O-Rings (19) seal the interior from the ambient atmosphere.
  • FIG. 17 is a cross-sectional view showing the body (1), orifice (20), the pole piece (3) and the armature sub-assembly (5), in order to even more clearly illustrate construction according to some embodiments.
  • the elastomeric insert (14) of the poppet (2) closes the internal opening of the orifice (20), preventing fluid flow therethrough.
  • FIG. 18 illustrates operation according to some embodiments.
  • a de-energized condition i.e., no electrical current flowing through the coil (18)
  • pre-loaded forces in the valve spring (7) push the poppet (2) against the end of the orifice (20) creating a seal.
  • current in the coil (18) Upon application of electrical current, current in the coil (18) generates magnetic flux along a path passing through the ferromagnetic housing (13), the pole piece (3), the armature (5) and the core (12), as shown.
  • This magnetic flux traverses the illustrated cylindrical radial air gap between the internal cylindrical surface of the pole piece (3) and the corresponding external surface of the armature (5) and the illustrated conical air gap between the internal surface of the armature (5) and the center portion of the pole piece (3).
  • the magnetic flux generates a net axial force across the conical air gap as illustrated, attracting the armature (5) towards the pole piece (3), and tending to lift the poppet (2) off the orifice (20). If the magnetic flux, and resulting axial force, is strong enough, the poppet (3) lifts off the orifice (20) and allows the working fluid to flow in through the center of the orifice (20) and out of the exit ports in the body (1).
  • the magnetic flux will also create radial forces as it crosses the radial air gap between the internal cylindrical surface of the pole piece (3) and the external cylindrical surface of the armature (5).
  • the radial forces will substantially cancel each other out if the armature (5) is kept concentric with respect to the pole piece (3) during operation. This concentricity is facilitated in some embodiments by the radial stiffness of the disk springs (4) and (7) and the tight tolerances of the internal features of the pole piece (3).
  • the increased axial force for a given amount of applied current enables the use of a stiffer combination of guide spring (4) and valve spring (7).
  • a stiffer combination of guide spring (4) and valve spring (7) results in more linear operation with less hysteresis than a less-stiff combination of guide spring (4) and valve spring (7).
  • the same guide spring may be used to provide a same linearity and hysteresis as less-efficient designs, but at a lower operating current.
  • the axial force will increase as the armature (5) gets closer to the pole piece (3).
  • the mating surfaces of both parts are conical in order to minimize this effect and to therefore increase linearity of a relationship between current and axial force, both during opening (i.e., lifting the poppet (2) off of the orifice (20)) and closing (i.e., allowing the poppet (2) to move toward the orifice (20)).
  • Some embodiments therefore provide a controlled opening between the orifice (20) and the poppet (2), substantially proportional to the electrical current passing through the coil (18), thus allowing improved fluid flow control.
  • FIG. 19 shows relationships between valve fluid flow and coil current according to some embodiments.
  • the magnetic force attracting the armature (5) to the pole piece (3) is less than the pre-load from the valve spring (7).
  • the orifice remains closed and only leakage flow passes threrethrough.
  • the magnetic force is sufficient to begin to lift the poppet (2) off the orifice (20) and flow starts to increase.
  • Increasing the coil current above the initial current value results in increasing fluid flow up to some maximum value dependent on the size of the orifice (20).
  • the flow characteristics can be selectively modified (e.g., for a given application) by changing the combined stiffness of, and the preload applied to, the valve spring (7) and the guide spring (4), and by changing the orifice opening.
  • FIGS. 20-22 illustrate effects on the relationship between fluid flow and coil current caused by each of these changes.
  • FIG. 20 shows that increasing the preload applied to the valve spring (7) increases the initial current value required for poppet lift-off and reduces the flow output for a given coil current.
  • FIG. 21 shows that increasing the combined stiffness of the disk springs (4) and (7) leaves the initial current value substantially unchanged, while reducing the slope of the current vs. flow characteristic curve.
  • FIG. 22 shows that increasing the orifice diameter decreases the initial current value required for poppet lift-off and increases the slope of the current vs. flow characteristic curve.
  • FIG. 23 also shows changes to the current vs. flow characteristic curve caused by changing the the orifice diameter.
  • FIG. 23 assumes that the orifice (20) is an outlet and that the incoming fluid arrives at a side port of the housing (1).
  • increasing the orifice diameter in such a case has an effect which is opposite from the reverse case illustrated in FIG. 22. That is, increasing the orifice diameter increases the initial current value required for poppet lift-off and decreases the flow output for a given coil current.
  • the threaded connection between the housing (13) and the body (1) may be designed to allow some degree of adjustment. Threading the housing (13) further into the body (1) has the effect of increasing the preload on the disk springs (4) and (7) and vice versa.
  • the preload may be adjusted in order to achieve a particular initial opening current for a particular inlet pressure. For example, during assembly, a current slightly above the initial opening current is applied to the coil (18) and the flow is monitored. The housing is then threaded in or out as appropriate to achieve a desired flow for a given current. Using this method, part-to-part variations can be minimized, and devices can be produced with more- consistent initial opening current or other characteristic(s).
  • the interface between the orifice (20) and the body (1) may be threaded in order to adjust the preload by threading the orifice (20) in and out of the body (1).
  • the velocity of the fluid passing between the orifice (20) and the poppet (2) causes flow reaction forces which tend to force the poppet (2) towards the orifice (20).
  • Some embodiments minimize these forces by designing the poppet (2) to have a much larger diameter than the orifice (20). This larger diameter forces the fluid to flow radially after exiting the orifice (20) and minimizes the (axial) flow forces.
  • Embodiments are not limited to the control of fluid flow.
  • the principles herein may be used to provide a linear motor and/or solenoid usable for any purpose.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • Magnetically Actuated Valves (AREA)

Abstract

La présente invention concerne un appareil pouvant comprendre un boîtier ferromagnétique définissant une cavité de boîtier, une bobine électroconductrice disposée dans la cavité de boîtier et définissant une cavité de bobine, une pièce centrale ferromagnétique disposée dans la cavité de bobine, une pièce de pôle ferromagnétique comprenant une première face en contact avec la pièce centrale et une partie saillante s'étendant depuis une seconde face de la pièce de pôle opposée à la première face, un élément flexible définissant une ouverture, la partie saillante étant disposée dans l'ouverture et l'élément flexible étant disposé entre une partie de la partie saillante et la première face de la pièce de pôle, et une armature ferromagnétique couplée à l'élément flexible, l'élément flexible étant disposé entre au moins une partie de l'armature et la première face de la pièce de pôle.
EP16752953.6A 2015-02-17 2016-02-17 Appareil solénoïde Active EP3259510B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201562117175P 2015-02-17 2015-02-17
PCT/US2016/018189 WO2016133974A1 (fr) 2015-02-17 2016-02-17 Appareil solénoïde

Publications (3)

Publication Number Publication Date
EP3259510A1 true EP3259510A1 (fr) 2017-12-27
EP3259510A4 EP3259510A4 (fr) 2018-10-31
EP3259510B1 EP3259510B1 (fr) 2020-01-15

Family

ID=56621345

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16752953.6A Active EP3259510B1 (fr) 2015-02-17 2016-02-17 Appareil solénoïde

Country Status (3)

Country Link
US (2) US9704636B2 (fr)
EP (1) EP3259510B1 (fr)
WO (1) WO2016133974A1 (fr)

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US20160240300A1 (en) 2016-08-18
EP3259510B1 (fr) 2020-01-15
US9620274B2 (en) 2017-04-11
WO2016133974A1 (fr) 2016-08-25
US20160240295A1 (en) 2016-08-18
EP3259510A4 (fr) 2018-10-31
US9704636B2 (en) 2017-07-11

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